期刊文献+

充气直管硬化对轴压承载力影响的研究

Research on the impact on the structural property by rigidization of the inflatable boom
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摘要 为了分析碾压铝箔薄膜硬化后充气管的轴压承载力,考虑层合薄膜的塑性变形在膜上产生初应力,并通过层合薄膜拉伸试验测出残余应变,基于该残余应变用ANSYS软件计算了1.2 m长充气管硬化后的承载力,得到硬化后承载力比硬化前提高了24%.并制作了一根1.2 m长的卷尺加劲充气管模型,进行了内部气压为0和0.02MPa两种情况下的轴压承载力实验,证明了分析方法的正确性. To research the axial-compressed load capacity of inflatable boom with rigidized laminated aluminum,the initial stress on the laminate with plastic deformation was taken account of,and the residual strain was gained by the tensile experiment of laminate. Using ANSYS program to calculate the axial load capacity of 1.2 meters long boom according to the residual strain, the mechanical properties unrigidized and rigidized were compared, which showed that the load capacity of rigidized one increased by 24%, then a 1.2 meters long boom model was developed, and experiments for axial load capacity under the pressure load 0 and 0. 02 MPa were carried out, proving that the analysis method is true.
作者 程亮 关富玲
出处 《工程设计学报》 CSCD 北大核心 2010年第4期268-272,共5页 Chinese Journal of Engineering Design
基金 民用航天科研预先研究项目(C1320060312)
关键词 层合薄膜 塑性变形 硬化 残余应变 laminate plastic deformation rigidizable residual strain
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参考文献8

  • 1管喻.充气展开自硬化支撑管的设计与研究[D].杭州:浙江大学空间结构研究中心,2006:15-30. 被引量:1
  • 2SEFFEN K A,PELLEGRINO S.Folding and deployment of curved tape springs[J].International Journal of Mechanical Sciences,2000,42(10):2055-2073. 被引量:1
  • 3FANG Hou-fei,LOU Michael,HUANG John.Inflatable structure for a three-meter reflectarray antenna[J].Journal of Spacecraft and Rockets,2004,41(4):543-550. 被引量:1
  • 4FANG Houfei,LOU Michael,HUANG John.Development of a 7-meter inflatable reflectarray antenna[C].AIAA Paper 2004-1502,the 45th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics & Materials Conference.California,2004. 被引量:1
  • 5FANG Hou-fei,HUANG John,UBALDO Quija.Design and technologies development for an eight-meter inflatable reflectarray antenna[C].AIAA Paper 2006-2230,the 47th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference.Rhode Island,2006. 被引量:1
  • 6韩智超..Kapton-Al-Kapton充气展开支撑管的结构参数设计与工艺研究[D].哈尔滨工业大学,2003:
  • 7周涛,谢志民,杜星文.空间充气支撑管的轴压屈曲分析[J].齐齐哈尔大学学报(自然科学版),2007,23(2):88-92. 被引量:1
  • 8叶武强..卷尺加劲可展自硬化充气管研究[D].浙江大学,2007:

二级参考文献6

  • 1Freeland R E,Bilyeu G D,Veal G R.Inflatable Deployable Space Structures Technology Summary[C].IAF-98-I.5.01:1-16. 被引量:1
  • 2Patrick K Malone,Geoffrey T Williams.Lightweight Inflatable Solar Array[J].Journal of Propulsion and Power,1996,12(5):866-872. 被引量:1
  • 3P M Beauchmap,D H Rodgers.New Concepts for Inflatable Structures Applied To Spaceborne Radars[C].AIAA-95-3795:1~8. 被引量:1
  • 4Shen H S.Post-buckling analysis of imperfect stiffened laminated cylindrical under axial compression[J].Computers and Structures,1997,62(3):335-348. 被引量:1
  • 5A H 奈弗著,王辅俊,徐均涛,谢寿鑫译.摄动方法[M].上海:上海科学技术出版社,1984:1-21. 被引量:1
  • 6Shen H S,Chen T Y.A boundary layer theory for the buckling of thin cylindrical shells under axial compression[A].Advances in Applied Mathematics Mechanics in China[C].Beijing:Academic Publishers,1990:155-172. 被引量:1

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